公开(公告)号：US11679886B2

公开(公告)日：2023-06-20

申请号：US17725641

申请日：2022-04-21

Applicant: Airbus Operations SAS

Inventor： Michael Berjot ,  Rémi Lansiaux ,  William Bras ,  Germain Gueneau ,  Sébastien Van Arendonk ,  Jacques Demange ,  Sébastien Commenge

IPC: B64D27/26 ,  B64D27/18 ,  F02C7/20

CPC classification number: B64D27/18 ,  F02C7/20 ,  B64D2027/268

Abstract: A linking device connecting an aircraft engine and a primary structure of an aircraft pylon, comprising a support connected to the primary structure, a spreader having a central part connected to the support and a first and a second end that are connected to thrust rods, at least one limiting system for limiting the travel of the spreader having an upper and a lower stop between which is positioned the first or second end of the spreader, the upper and the lower stop being connected to one another so as to form a single part connected to a fitting secured to the support.